View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 15056.50203388 -.00000009 00000-0 27677-4 0 9997
2 24278 098.5280 040.4670 0350303 000.6073 107.8814 13.53045226914923
| Epoch (UTC): | 25 February 2015 12:02:55 |
| Eccentricity: | 0.0350303 |
| inclination: | 98.5280° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 40.4670° |
| argument of perigee: | 0.6073° |
| revolutions per day: | 13.53045226 |
| mean anomaly at epoch: | 107.8814° |
| orbit number at epoch: | 91492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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